US2005244215A1PendingUtilityA1

Assembly of structural parts

Assignee: AIRBUS FRANCEPriority: Apr 28, 2004Filed: Apr 22, 2005Published: Nov 3, 2005
Est. expiryApr 28, 2024(expired)· nominal 20-yr term from priority
Y10T403/473F16B 11/006
40
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Claims

Abstract

Assembly of structural parts. The method of assembly consists in: laying a layer of adhesive material between facing surfaces of said parts, forming an assembly plane; and inserting and bonding, in a hole made in said structural parts transversely to said assembly plane, a joining element consisting of a peg made of a material similar to that of said structural parts.

Claims

exact text as granted — not AI-modified
1 . A method of assembling at least two structural parts ( 1 ,  2 ) along an assembly plane, this method consisting in: 
 laying a layer of adhesive material ( 3 ) between facing surfaces of said parts, forming said assembly plane; and    inserting and bonding, in a hole ( 10 ) made in said structural parts transversely to said assembly plane, a joining element ( 11 ) consisting of a peg ( 12 ) made of a material similar to that of said structural parts.    
     
     
         2 . The method as claimed in  claim 1 , wherein at least one transverse end face ( 14 ) of said peg ( 12 ) is made flush with an external surface of one of said structural parts ( 1 ,  2 ).  
     
     
         3 . An assembly of at least two structural parts ( 1 ,  2 ) along an assembly plane, in which facing surfaces of said parts, forming said assembly plane, are bonded together and a joining element ( 11 ), consisting of a peg ( 12 ) made of a material similar to that of said structural parts ( 1 ,  2 ) is bonded in a hole ( 10 ) made in said structural parts transversely to said assembly plane.  
     
     
         4 . The assembly as claimed in  claim 3 , wherein at least one transverse end face ( 14 ) of said peg ( 12 ) lies flush with an external surface of one of said structural parts ( 1 ,  2 ).

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